Path: csiph.com!eternal-september.org!feeder.eternal-september.org!nntp.eternal-september.org!.POSTED!not-for-mail From: Christopher Howard Newsgroups: sci.physics Subject: Re: force generated by propeller? Date: Mon, 02 Feb 2026 07:36:19 -0900 Organization: A noiseless patient Spider Lines: 24 Message-ID: <87jywvdrwc.fsf@librehacker.com> References: <87h5s2iyw7.fsf@librehacker.com> <10lmot1$l7fi$1@gwaiyur.mb-net.net> MIME-Version: 1.0 Content-Type: text/plain Injection-Date: Mon, 02 Feb 2026 16:36:20 +0000 (UTC) Injection-Info: dont-email.me; posting-host="7729e7c5fa919ea81d758209eff22745"; logging-data="818522"; mail-complaints-to="abuse@eternal-september.org"; posting-account="U2FsdGVkX18lD5jXwqxyE05CXWWcWFWSMKNqytA+Xus=" User-Agent: Gnus/5.13 (Gnus v5.13) Cancel-Lock: sha1:hpQafCGcvR/YyvKNp3K0sbVLyNk= sha1:0ZGcX3SFsFSSVcqoCK14WcXvkzg= Xref: csiph.com sci.physics:895030 Thomas 'PointedEars' Lahn writes: > Christopher Howard wrote: >> I was wondering if it was possible, without diving too deeply into the >> math and details, to roughly figure out the lbf that can be generated by >> a propeller with, > > What do you mean by "the lbf that can be generated"? With the wikipedia articles on jet aircraft, there is usually listed the pounds-force thrust that is generated by each of the engines, which along with the empty weight (or whatever additional weight you want to add) can be used easily to calculate the thrust-to-weight ratio. Some fighter aircraft achieve 1:1 but most commercial jets are somewhere around 0.6 to 0.7, from what I can tell. In the specs I was seeing for propeller aircraft, it seems what is usually listed is weight-per-horsepower, or power loading. That is interesting, but I was having trouble seeing how to compare the two. Thrust is more intuitive to me one can see directly the ratio between thrust lbf and weight lbs. -- Christopher Howard